Valentin - Consultant MS OFFICE

Expérience professionnelle

Jun 2014 – present POTEZ/Dassault (contract) Toulouse/France
Aerospace Design Engineer

Dassault Falcon 5X – Aerospace Design Engineer, PAX Door Project

Responsibilities:

• Design of the structure, mechanisms and kinematics for Dassault Falcon 5X PAX Door.
o Development of door mechanism kinematics, path generators, movement generators and kinematic chain (actuators, cams, cranks, rods, etc.)
o Analysis and synthesis of linkages
o Dimensional and kinematic synthesis
• Ergonomic analyses of door function
• Preliminary design layout, detail drawings and interface drawings




Jan 2013 – Feb 2014 CEiiA/EEA (contract) Porto - Portugal
Lead Engineer

KC 390 Military Cargo Lifter – Design Lead of the KC 390 Sponson Project

Responsibilities:

• Provide design engineering guidance
• Ensure delivery of all drawings and reports according schedule
• Review of drawings before final release
• Detail coordination with client manufacturing, design staff and material engineer supporting the design development and drawing release schedule of KC-390 program
• Support for the program management team with visibility of status inputs related to drawing release
• Planning and progress tracking of detail design tasks related to different phases of design development program
• Support for technical integrator in resolving design related pending issues impeding drawing release drawing schedule

Achievements:

• Successfully leading a team of 30 design engineers and delivered the work-package within the agreed deadline.
• Mentoring and training of the junior design engineers.
• Technical evaluation of the suppliers proposals/ answers to calls for tender; evaluated the impact of various technical solutions with regards to cost and impact on project schedule




Aug. 2011 – September 2012 Bombardier/SAC (contract) Shenyang - China
Aerospace Design Engineer

CSERIES project - part of the CSERIES Door Surround team, responsible with conceptual/ detailed design layouts, 3D design, 2D drafting and installations of PAX, cargo and service doors Primary & Secondary structure – frames, lintels, intercostal, door stoppers and, sheet metal
/machined parts and assemblies for the primary and secondary aircraft structure.

Responsibilities:

• Door Surround primary/ secondary structure conception/detail design.
• Manage design modifications.
• Liaise with Stress/Production/Systems teams to ensure optimum design solutions.
• Provided technical support for client/ suppliers.




Jan. 2010 – Aug. 2011 SkyAircraft SAS Chambley - France
Aerospace Design Engineer

SK-105 SKYLANDER project - part of the Skylander SK 105 Fuselage/Wing Structure design team, responsible with design of conceptual design layouts, 3D design, 2D drafting and installations of Primary & Secondary structure - composite flap track fairings, skin panels, frames, stringers and, sheet metal /machined parts and assemblies for the primary and secondary aircraft structure.

Responsibilities:

• Primary/ secondary structure conception design.
• Manage design modifications
• Liaise with Production/Systems teams to ensure optimum design solutions
• Provide technical support for suppliers




Jan. 2009 – Nov. 2009 Hyde Group UK (contract) Hamburg - Germany
Aerospace Design Engineer

Part of the A380 DQN team in Hamburg , responsible with investigating (Dvise - mock-up), managing and incorporating design modification in to 2D (drawings - Catia V4) and highlight, manage BOM modifications (GILDA) - for electrical routing ( harnesses) and electrical fix supports.

Responsibilities:

• Incorporate inputs from Production Line into Catia V4 2D/GILDA/ECN.
• Implement electrical design queries notes (DQNs) into the latest production design solution.
• Manage design modifications
• Liaise with MAP team to ensure optimum design solutions
• Provide technical support for client


Apr. 2008 – Nov. 2008 ASSYSTEM Romania Bucharest - Romania
Team leader

A330 -GMF SFX Project for Assytem France ( Sections S12, S15 lower & upper shell, NLGB) - designing, modifying fix supports ( brackets) in concordance with provided inputs (interface points), apply appropriate Airbus standards and specification for bracket installation,fixations; creation and modification of 2D bracket and installation drawings (CADDS5); BOM creation and management (GILDA).

Responsibilities:

• Manage a team of 3-5 designers
• Planning, organizing and assure technical support and expertise




Nov. 2003 – Apr.2008 GECI Engineering Services Bucharest - Romania
Senior Design Engineer

GECI Engineering Services is part of GECI International, a technology engineering company offering various engineering services such as design, calculations, qualification, systems, integration, and tests.

Responsibilities:

• Provide technical expertise for different international clients
• Execute various design projects
• Technical solutions proposal

Various national and international projects for different GECI Engineering Services clients, such as:

Dates Client/Projects Location

Dec 07- Apr 08 Airbus SAS Bucharest - Romania
Senior Design Engineer - Pylon A350 XWB Demonstrator

Joined Phase and Definition Phase: Finished Design for maturity phase A, creation of:

• 2D Drawings, batch 2 and 3 for elementary parts and assemblies,
• Creation of MRG- Geometrical Reference Model for Pylon A350 XWB Demonstrator.



Jul. 05 - Dec. 07 Geci France Bucharest- Romania
Senior Design Engineer - Airbus A400M-Ramp Project

• Check and create 2D drawings and Bill of Materials for Equipped brackets and structure assemblies from Airbus A400M Ramp project


Jun. 05 - Jul. 06 Airbus SAS Toulouse- France
Senior Design Engineer - Airbus A350 Cockpit & Nose Fuselage

Working on A350 Front Fuse Primary structures team. Responsible for generation of conceptual design layouts, 3D design, 2D drafting and installations of Primary & Secondary structure. (Catia V5 & Primes)

• Research and developed new solutions
• Provide technical expertise
• Implemented double curved lateral window
• Improved new floor strcture design (gain a 10% weight reduction)
• Liaise and ensure interfaces with the Airframe, Landing Gear and Systems Design & Stress Teams in order to establish optimum design solutions




Mar. 2003 - Sep.2003 National Centre for Research of Technological
Systems Performances “OPTIMUM” Bucharest - Romania
Trainer